Publisher
American Institute of Aeronautics and Astronautics
Reference7 articles.
1. Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor
2. I Russler, P.M., Rabe, D. C., Cybyk, B. Z. and Hah, C., 1995, "Tip Flow Fields in a Low Aspect Ratio Transonic Compressor," ASME Paper No. 95-GT089.
3. Cybyk. B. Z, Rabe, D. C., Russler, P. M. and Hah, C. "Characterization of the First-Stage Rotor in a Two StageTransonicCompressor,"AIAA-95-2460
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